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4) Wipe off excess sealant with a clean lintfree cloth moistened with cleaning agent (TB 11-003).
5) Position coverplate (7) and install rivets - refer to 51-40-02.
6) Perform paint touch-ups - refer to 20-00-03.
7) Position electrical harness (9) and install harness holding clips (8) on coverplate (7).
8) Connect the electrical wiring of stall warning device - voir 27-30-04.
9) Make sure all the tools and materials are removed and the work area is clean and free from debris.
10) Install the wing tip - refer to 57-30-00.
11) Install the inspection door 516 [616] - refer to 52-40-00.
12) Install the ailerons - refer to 57-60-00.
WA
Validity : S / N 1 - 9999 57-20-00Page 403
(BA) SEP 04
1 - Arm assembly
2 - Bolt
3 - Washer
4 - Nut
5 - Arm assembly
6 - Arm assembly
7 - Coverplate
8 - Harness holding clip
9 - Electrical harness
10 - Arm assembly
11 - Bolt
12 - Washer
13 - Nut
WA
Validity : S / N 1 - 9999 57 20 00Page 404
(BA) JUN 02
WING FITTINGS
REMOVAL / INSTALLATION
NOTE : This procedure is applicable to L.H. and R.H. installations. Information specific to R.H. installation are given in square brackets.
1. REMOVAL OF THE WING FRONT ATTACHMENT (Figure 401)
A. Tools and consumable materials
- 1 padded support for frame C8
- 2 wing padded supports, P / N TB10 99000911
- Cleaning agent (TB 11-003)
- Spatula
- Clean lintfree cloths
B. Procedure
1) Remove the cowling under hull 218 F.
2) Remove junction fairing 217L [217R].
CAUTION : TO AVOID DAMAGING THE STRUCTURE, THE SUPPORTS MUST PERFECTLY FIT THE FUSELAGE PROFILE AND HAVE PADDED BEARING AREAS.
3) Install padded supports under the L.H. and R.H. wings at a rib, and under the rear fuselage at frame C8.
4) Remove and discard nut (2), remove washer (1), shim (4) and bolt (5).
5) Remove and discard nuts (9), remove washers (8) and bolts (10).
6) Remove and retain front fitting (3).
7) Remove the sealant with a spatula and clean the surfaces with a clean lintfree cloth moistened with cleaning agent (TB 11-003).
8) If necessary, check front fitting (3) - refer to Page 601.
2. INSTALLATION OF THE WING FRONT ATTACHMENT (Figure 401)
A. Tools and consumable materials
- 1 padded support for frame C8
- 2 wing padded supports, P / N TB10 99000911
- Grease (TB 04-004A)
- Petrolatum (TB 04-012)
- Red paint
- Torque wrench 0 - 885 lbf.in (0 - 100 N.m)
- Sealant (TB 09-916)
- Cleaning agent (TB 11-003)
ACAA
Validity : S / N 1 - 9999 57-20-03Page 401
(DA) SEP 04
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